CN111344902A - Millimeter wave radar cover - Google Patents

Millimeter wave radar cover Download PDF

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Publication number
CN111344902A
CN111344902A CN201980005647.4A CN201980005647A CN111344902A CN 111344902 A CN111344902 A CN 111344902A CN 201980005647 A CN201980005647 A CN 201980005647A CN 111344902 A CN111344902 A CN 111344902A
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China
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millimeter wave
millimeter
wave
laminated structure
antenna
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CN201980005647.4A
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CN111344902B (en
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山田武司
多田健人
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Nok Corp
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Nok Corp
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/93Radar or analogous systems specially adapted for specific applications for anti-collision purposes
    • G01S13/931Radar or analogous systems specially adapted for specific applications for anti-collision purposes of land vehicles
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/027Constructional details of housings, e.g. form, type, material or ruggedness
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/32Adaptation for use in or on road or rail vehicles
    • H01Q1/3208Adaptation for use in or on road or rail vehicles characterised by the application wherein the antenna is used
    • H01Q1/3233Adaptation for use in or on road or rail vehicles characterised by the application wherein the antenna is used particular used as part of a sensor or in a security system, e.g. for automotive radar, navigation systems
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome
    • H01Q1/422Housings not intimately mechanically associated with radiating elements, e.g. radome comprising two or more layers of dielectric material
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome
    • H01Q1/425Housings not intimately mechanically associated with radiating elements, e.g. radome comprising a metallic grid
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/52Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure
    • H01Q1/526Electromagnetic shields
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/0006Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices
    • H01Q15/0013Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices said selective devices working as frequency-selective reflecting surfaces, e.g. FSS, dichroic plates, surfaces being partly transmissive and reflective
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/02Refracting or diffracting devices, e.g. lens, prism
    • H01Q15/08Refracting or diffracting devices, e.g. lens, prism formed of solid dielectric material
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/03Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • General Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Computer Security & Cryptography (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aerials With Secondary Devices (AREA)
  • Details Of Aerials (AREA)
  • Support Of Aerials (AREA)
  • Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)

Abstract

Provided is a cover for a millimeter wave radar, which can effectively utilize electromagnetic waves (millimeter waves) of a millimeter wave radar and can sufficiently suppress unnecessary electromagnetic wave radiation. A millimeter-wave radar cover (1) houses a millimeter-wave radar including an antenna (30) and an electronic circuit (40) for driving the antenna (30), and a first part (A) which protects the millimeter wave radar and is provided on the front surface of the millimeter wave radar so as to transmit the millimeter waves emitted from the antenna (30), and a second part (B) which has a storage space for storing the antenna (30) and the electronic circuit (40) excluding the first part (A), wherein the first part comprises a laminated structure (10), the laminated structure (10) is formed by laminating at least one layer of a first structural member (11) having a negative relative permittivity in a millimeter wave frequency band and at least one layer of a second structural member (12) having a positive relative permittivity in the millimeter wave frequency band, and the laminated structure (10) is curved in a convex shape in a direction away from a transmission source with the transmission source of a millimeter wave electromagnetic wave as a center.

Description

Millimeter wave radar cover
Technical Field
The present invention relates to a cover for a millimeter wave radar, and more particularly, to a cover for a millimeter wave radar that houses a millimeter wave radar for a vehicle that can realize automatic travel of an automobile or the like.
Background
Conventionally, a millimeter wave radar for vehicle use is constituted by an antenna for receiving and transmitting an electromagnetic wave, and an electronic circuit including a drive circuit for driving the antenna and a power supply.
The size (dimension) of an antenna that receives and transmits an electromagnetic wave depends on the form of the antenna, but in many cases, the higher the frequency of the electromagnetic wave, the shorter the wavelength, and therefore the higher the frequency, the smaller the wavelength for the same form of antenna. Further, as electronic circuits, integration and miniaturization have been progressing due to advances in semiconductor technology, and rapid miniaturization has been progressing without being limited to this field.
In contrast, in the electronic circuit-mounted product of the age in which the conventional low-frequency radar product and/or the semiconductor technology has not progressed so much, the antenna and the electronic circuit are disposed in different cases, and even if the antenna and the electronic circuit are disposed in the same case, the antenna and the electronic circuit are often disposed independently in the case.
There has been proposed a radome in which an antenna and an electronic circuit, which are electronic components of a millimeter wave radar, can be housed in the same case by downsizing the antenna and the electronic circuit (see, for example, patent document 1).
In this way, the antenna and the electronic circuit can be housed in the same case or mounted in a state close to each other, and therefore, it is difficult to physically separate the antenna and the electronic circuit, and the boundary between the antenna and the electronic circuit becomes unclear.
On the other hand, in designing a case for housing the components of these millimeter wave radars, it is necessary to consider the electromagnetic wave propagation characteristics of the case from the viewpoint of effective use of electromagnetic waves (millimeter waves) and from the viewpoint of suppression of unnecessary electromagnetic wave radiation required for electronic devices.
When the antenna and the electronic circuit are disposed in separate housings or are disposed independently of each other as in the conventional art, the housings may be designed individually in consideration of both the effective use of the millimeter-wave radar and the suppression of unnecessary electromagnetic radiation.
However, the miniaturization of antennas and electronic circuits has been progressing, and it has been difficult to design a case that satisfies both a viewpoint of effective use of electromagnetic waves (millimeter waves) and a viewpoint of suppressing radiation of unnecessary electromagnetic waves required for electronic devices in recent millimeter wave radars in which antennas and electronic circuits are mounted in a state of being very close to each other.
Specifically, the requirements for the transmission or shielding properties of electromagnetic waves with respect to the housing material vary depending on the location of the millimeter wave radar, and therefore the design specifications of the housing material vary depending on the location. Fig. 17 summarizes the desired design specification as being divided into location A, B and frequency band I, II.
The portion is divided into two portions, i.e., a portion a (a portion corresponding to a radome in the radar) for receiving the transmitted electromagnetic wave (millimeter wave) and a remaining portion B for accommodating the millimeter wave radar except the portion a, from the viewpoint of transmitting and shielding the millimeter wave used as the millimeter wave radar.
The frequency to be considered for design is functionally divided into two frequency bands, I (76.5GHz) in the millimeter wave band used as an Electromagnetic wave and II (about 1GHz or less) in the wide frequency band in which suppression of unnecessary Electromagnetic wave radiation and intrusion of Electromagnetic waves from the outside is considered, particularly in the EMC (Electromagnetic Compatibility) region (noise countermeasure region) of 1GHz or less. The frequency band I in the millimeter wave band is not limited to 76.5GHz, and may be arbitrarily set in the range of 76GHz to 81 GHz.
Considering the portion A, B, the frequency band I (76.5GHz), and the frequency band II (about 1GHz or less), the transmittance T of the electromagnetic wave to the case material needs to be set for the portion A, B, the frequency band I (76.5GHz), and the frequency band II (about 1GHz or less).
For example, in the region AI of the region a and the frequency band I (about 76.5GHz or less), it is necessary to transmit the electromagnetic wave of the millimeter wave in order to realize the radar function of the millimeter wave radar, and therefore, it is desirable that the transmittance T of the case material for the electromagnetic wave be "1". Here, the transmittance T of "1" means a state of the casing material in which the casing material transmits electromagnetic waves.
In particular, in the case of radar applications, theoretically, electromagnetic waves attenuate in proportion to the square of the distance between the antenna of the millimeter wave radar and the object. Therefore, when considering the reciprocating distance that returns after being transmitted from the antenna and reflected by the object, the electromagnetic wave is attenuated in proportion to the fourth power of the distance, and the transmittance T of the housing material greatly affects the performance (detection sensitivity, accuracy, precision) of the product.
For example, in a region BI in a region B and a frequency band I (76.5GHz), it is functionally unnecessary to transmit electromagnetic waves of millimeter waves, and it is desired to prevent the penetration of millimeter waves in order to prevent interference and interference of electromagnetic waves from other external devices. That is, in order to shield the electromagnetic wave of the millimeter wave, it is desirable that the transmittance T of the case material be "0". Here, the transmittance T of "0" means a state of full shielding in which the casing material does not transmit electromagnetic waves at all.
In the region AII of the portion a and the band II (about 1GHz or less) and the region BII of the portion B and the band II (about 1GHz or less), from the viewpoint of suppressing unnecessary electromagnetic radiation, it is desirable that the transmittance T of the case material be "0" in order to shield the electromagnetic wave of the band II (about 1GHz or less) in the EMC region from transmitting therethrough.
Documents of the prior art
Patent document
Patent document 1 Japanese patent laid-open No. 2013-102512
Disclosure of Invention
Technical problem to be solved by the invention
In the region a of the housing of the millimeter wave radar having the above-described configuration, it is desirable that the transmittance T of the housing material in the frequency band I (76.5GHz) be "1" and the transmittance T of the housing material in the frequency band II (about 1GHz or less) be "0", and completely opposite characteristics are required depending on the frequency band I (76.5GHz) and the frequency band II (about 1GHz or less).
However, a housing material that satisfies such opposite characteristics at the same time is not present. Therefore, conventionally, in consideration of the wavelength shortening effect due to the relative permittivity of the casing material, a casing having a thickness of an integral multiple of half wavelength of the electromagnetic wave to be used is used, and the design is performed such that the transmittance T of the casing material for the electromagnetic wave of the frequency band I (76.5GHz) is set to "1" and the function as a radar is prioritized, while the design is hardly considered with respect to the transmittance T of the casing material for the electromagnetic wave of the frequency band II (about 1GHz or less) being set to "0".
Therefore, although effective use of electromagnetic waves of millimeter wave radars is possible in a case made of a conventional material, it is difficult to sufficiently suppress radiation of unnecessary electromagnetic waves required for electronic devices.
The present invention has been made in view of the above-described problems, and an object thereof is to provide a cover for a millimeter wave radar which can effectively utilize electromagnetic waves of a millimeter wave radar, can sufficiently suppress radiation of unnecessary electromagnetic waves, and can prevent intrusion of unnecessary electromagnetic waves from the outside.
Means for solving the problems
In order to achieve the above object, the present invention provides a cover for a millimeter wave radar that houses a millimeter wave radar having an antenna and an electronic circuit for driving the antenna, the cover comprising: a first portion that protects the millimeter wave radar and is provided on a front surface of the millimeter wave radar so as to transmit an electromagnetic wave of a millimeter wave emitted from the antenna; and a second portion having a housing space for housing the antenna and the electronic circuit, excluding the first portion, wherein the first portion includes a laminated structure in which at least one layer of a first structural member having a negative dielectric constant in the millimeter wave band and a second structural member having a positive dielectric constant in the millimeter wave band is laminated, and the laminated structure is bent in a convex shape with a source of the electromagnetic wave of the millimeter wave as a center in a direction away from the source.
In the millimeter wave radar cover according to the present invention, it is preferable that the multilayer structure has an apparent transmittance of about 1 only when the millimeter wave electromagnetic wave is incident perpendicularly.
In the millimeter-wave radar cover according to the present invention, it is preferable that the laminated structure is integrated with a dielectric lens having a predetermined dielectric constant and refracting the electromagnetic wave of the millimeter wave incident from the emission source.
In the millimeter wave radar cover according to the present invention, it is preferable that the first structural member is formed by geometrically arranging a conductive material, and when the first structural member and the second structural member are laminated, an apparent transmittance of the laminated structural body with respect to a frequency band of the millimeter wave is a value in the vicinity of 1.
In the millimeter wave radar cover according to the present invention, it is preferable that the multilayer structure has an apparent transmittance of a frequency band in an EMC (Electromagnetic Compatibility) region lower than the frequency band of the millimeter wave of a value in the vicinity of 0.
ADVANTAGEOUS EFFECTS OF INVENTION
According to the present invention, it is possible to realize a cover for a millimeter wave radar that can effectively utilize electromagnetic waves of a millimeter wave radar, sufficiently suppress radiation of unnecessary electromagnetic waves, and prevent intrusion of unnecessary electromagnetic waves from the outside.
Drawings
Fig. 1 is a schematic perspective view showing the entire configuration of a millimeter wave radar cover according to an embodiment of the present invention.
Fig. 2 is a schematic cross-sectional view showing the millimeter-wave radar cover, and an antenna and an electronic circuit housed therein.
Fig. 3 is a schematic perspective view and a schematic cross-sectional view showing a first structural member and a second structural member of a laminated structural body constituting a radome of a millimeter wave radar cover.
Fig. 4 is a schematic perspective view showing the structure of the second structural member made of a mesh-like conductive material.
Fig. 5 is a schematic diagram for explaining transmittance and reflectance.
Fig. 6 is a graph showing a relationship between a relative dielectric constant and a frequency of an electron conductive material.
Fig. 7 is a graph showing a relationship between a relative dielectric constant and a frequency of a conductive material formed in a grid shape.
Fig. 8 is a graph showing the calculation results of the relative permittivity and the relative permeability of the laminated structure.
Fig. 9 is a graph showing the transmittance of the laminated structure.
Fig. 10 is a sectional view showing the structure of the curved laminated structure.
Fig. 11 is a schematic diagram for explaining oblique incidence transmittance characteristics of the electromagnetic wave of millisecond wave to the curved laminated structure.
Fig. 12 is a graph showing oblique incidence transmittance characteristics of a millimeter wave electromagnetic wave with respect to a curved laminated structure.
Fig. 13 is a sectional view showing the structure of the dielectric lens integrated multilayer structure having a curved shape.
Fig. 14 is a schematic diagram for explaining oblique incidence transmittance characteristics of millimeter-wave electromagnetic waves with respect to a dielectric lens integrated multilayer curved structure.
Fig. 15 is a schematic diagram for explaining oblique incidence transmittance characteristics of millimeter-wave electromagnetic waves with respect to a dielectric lens integrated multilayer curved structure.
Fig. 16 is a cross-sectional view showing a structure of a dielectric lens integrated multilayer structure having a curved shape in accordance with another embodiment.
Fig. 17 is a graph showing the transmittance required for each of the portion A, B of the millimeter wave radome and the frequency band I, II.
Detailed Description
< embodiment >
Hereinafter, embodiments of the present invention will be specifically described with reference to the drawings. For convenience of explanation, in fig. 1 and 2, the front side of the millimeter wave radar cover 1 is indicated by an arrow a, and the rear side is indicated by an arrow b.
< integral Structure of cover for millimeter wave Radar >
As shown in fig. 1 and 2, the millimeter wave radar cover 1 is a housing that houses and protects an antenna 30 and an electronic circuit 40 from the outside, the antenna 30 receives and transmits electromagnetic waves of, for example, 76.5GHz in a millimeter wave frequency band (30 to 300GHz) as a transmission source, and the electronic circuit 40 includes a drive circuit, a power supply, and the like that drive the antenna 30.
The millimeter wave radar cover 1 includes a first portion A corresponding to an antenna cover disposed on the front surface of an antenna 30 that receives and transmits electromagnetic waves; and a second portion B corresponding to a closed-end prismatic cylindrical housing portion having a housing space (housing the antenna 30 and the electronic circuit 40) formed therein, excluding the first portion a.
As shown in fig. 3 (a) and (B), a three-layer laminated structure 10 is used in the first portion a of the millimeter wave radar cover 1, and the three-layer laminated structure 10 is formed by laminating a first structural member 11 and a second structural member 12 sandwiching the first structural member 11 from both the front side (the direction of arrow a) and the back side (the direction of arrow B).
The second portion B of the millimeter wave radar cover 1 is made of a shielding material made of a metal such as iron or a composite material obtained by plating a metal such as a resin, and suppresses radiation of unnecessary electromagnetic waves from the electronic circuit 40, thereby preventing interference or interference from external electronic equipment. That is, the transmittance T of the second portion B is "0" in both the millimeter wave band I (76.5GHz) and the EMC region band II (about 1GHz or less).
Note that, as described above, in the first region a, it is necessary to pass millimeter waves in order to realize the radar function of the millimeter wave radar in the frequency band I (76.5GHz) of the millimeter wave band, and therefore it is desirable that the transmittance T of the laminated structure 10 for electromagnetic waves be "1". On the other hand, in the second portion B, in a frequency band II (about 1GHz or less) of the EMC region (noise countermeasure region), the transmittance T of the laminated structure 10 is desirably "0" in order to shield the electromagnetic wave from transmission in order to suppress the radiation of the unnecessary electromagnetic wave.
< Structure of laminated Structure >
As described above, the first site a is required to have completely opposite characteristics such that the transmittance T becomes "1" in the millimeter wave frequency band I (76.5GHz) and the transmittance T becomes "0" in the EMC region frequency band II (about 1GHz or less). Since there is no material that satisfies this contrary requirement, the use of the laminate structure 10 as an artifact is decided in the present invention.
As shown in fig. 3, the first structural member 11 and the second structural member 12 are used in the laminated structure 10 as a case that satisfies both "1" for the transmittance T apparent in the millimeter wave frequency band I (76.5GHz) and "0" for the transmittance T apparent in the EMC region frequency band II (about 1GHz or less). However, the transmittance T is always only a theoretical value, and as a value that can be actually realized and evaluated, the transmittance T is set to a value in the vicinity of 1 where the transmittance T is 0.95(-0.45dB) or more for 1, and the transmittance T is set to a value in the vicinity of 0 where the transmittance T is 0.1(-20dB) or less for 0.
As shown in fig. 3 (a) and (B), the laminated structure 10 in this case is a three-layer sandwich structure formed integrally by an adhesive or the like with the first structural member 11 interposed between the second structural member 12 disposed on the front surface side (in the direction of arrow a) and the second structural member 12 disposed on the back surface side (in the direction of arrow B). However, the present invention is not limited to this, and may be a multilayer laminated structure in which at least one layer of the second structure 12 and the first structure 11 can be laminated, or two layers, or four or more layers of the second structure 12 and the first structure 11 can be laminated.
As shown in fig. 4, the first structural member 11 has a rectangular shape as a whole, and is made of an electrically conductive material such as copper (metal), for example, and is formed in a mesh shape such as a screen door using a metal wire of copper, for example. The first structural member 11 is not limited to a rectangular shape, and may have various other shapes such as a circular shape and an elliptical shape depending on the shape of the radar. The conductive material of the first structural member 11 is not limited to all metals such as copper, and may be carbon, a conductive polymer, or the like, or a material in which these are blended (metal, carbon, conductive polymer, or the like) with a resin, rubber, elastomer, or the like to impart conductivity.
Specifically, the first structural member 11 determines the size, number, and the like of the mesh by the thickness t of the frame forming the mesh, the frame width d, and the arrangement interval a of the frames. The arrangement interval "a" is a distance between the inner ends of the frames adjacent to each other to form the mesh, but is not limited thereto, and may be an inter-center distance between the center of the frame and the center of the frame.
The second structural member 12 is formed of a dielectric material such as resin (for example, polyimide, polytetrafluoroethylene, polyethylene, or the like) or rubber having material strength and resistance necessary for the housing of the millimeter wave radar cover 1. The second structural member 12 has a rectangular shape as a whole, and has the same size as the first structural member 11 or a slightly larger size so as not to expose the first structural member 11, as in the first structural member 11.
Here, as shown in fig. 5, since the laminated structure 10 is disposed in a free space, the electromagnetic wave radiated from the antenna 30 is reflected at both interfaces of the front surface side (arrow a direction) 10a of the laminated structure 10 and the inner surface 10b of the laminated structure 10.
In such a situation, the transmittance T of the laminated structure 10 disposed in the free space is determined by the wave impedance η of different substances such as air and the laminated structure 10 as shown in the following expression (1), that is, the transmittance T of the laminated structure 10 is determined by the wave impedance η 1 of the free space (air) and the wave impedance η 2 equivalent to the laminated structure 10, and the reflectance Γ is (η 2- η 1)/(η 2+ η 1).
T=1+Γ
=1+(η2-η1)/(η2+η1)
=2·η2/(η2+η1)………………………………………………………(1)
T: transmittance of light
F: reflectivity of light
η 1 wave impedance of incident side material (air)
η 2 wave impedance of the outgoing side substance (laminated structure 10)
Therefore, according to the equation (1), if the wave impedance η 1 of the incident-side substance (air) is made equal to the wave impedance η 2 of the exit-side substance (laminated structure 10), the transmittance T can be made equal to 1, which means that conversely, if the wave impedance η 2 of the exit-side substance (laminated structure 10) is smaller than the wave impedance η 1, the transmittance T can be made approximately equal to 0.
Here, the wave impedance η is determined by the dielectric constant and the magnetic permeability of the substance, and is represented by the following formula (2).
Figure BDA0002484089750000091
μ 0: magnetic permeability of vacuum
μ r: relative magnetic permeability
ε 0: dielectric constant of vacuum
ε r: relative dielectric constant
Therefore, the wave impedance η 1 of the incident-side substance (air) is represented by the following formula (3), and the wave impedance η 2 of the outgoing-side substance (laminated structure 10) is represented by the following formula (4).
Figure BDA0002484089750000092
Figure BDA0002484089750000093
As described above, since the wave impedances η 1, η 2 are expressed by the expressions (3) and (4), the transmittance T is determined by the relative permeability μ r1 and the relative permittivity ∈ r1 of the free space (air), and the equivalent relative permeability μ r2 and the relative permittivity ∈ r2 of the laminated structure 10.
Here, in equation (3), when both the relative permeability μ r1 and the relative permittivity ∈ r1 of the free space (air) are regarded as substantially "1", if the equivalent relative permeability μ r2 and the relative permittivity ∈ r2 of the laminated structure 10 are the same value, the wave impedance η 1 of the air and the equivalent wave impedance η 2 of the laminated structure 10 become the same value, and the transmittance T can be achieved to 1.
Conversely, if the ratio of the equivalent relative permeability μ r2 to the relative permittivity ∈ r2 of the laminated structure 10 is small, that is, if the relative permittivity ∈ r2 as the denominator is a negative value and has a large absolute value, the wave impedance η 2 approaches "0", and therefore the transmittance T can be achieved to be 0.
However, the relative permeability μ r of the nonmagnetic material has a value of approximately 1, but even the lowest polytetrafluoroethylene has a relative permittivity ∈ r of 2 as an industrial material of the nonmagnetic material generally used, and in order to make the relative permittivity ∈ r equal to the relative permeability μ r, it is necessary to increase the relative permeability μ r by blending a magnetic material. However, the magnetic material is not suitable for use because of a large loss of electromagnetic waves, and similarly, the magnetic material alone is not suitable for use.
Therefore, in the present invention, the laminated structure 10 is formed by: the laminated structure 10 in which the first structural member 11 made of an artificial material having a negative relative permittivity ∈ r in the millimeter wave frequency band I (76.5GHz) and the second structural member 12 having a normal positive relative permittivity ∈ r in the millimeter wave frequency band I (76.5GHz) are laminated can be set so that the equivalent relative permeability μ r2 of the laminated structure 10 is equal to the relative permittivity ∈ r 2.
In the multilayer structure 10, it is necessary to match the equivalent relative permittivity ∈ r of the multilayer structure 10 to 1 in the millimeter wave frequency band I (76.5GHz), and to increase the absolute value of the equivalent relative permittivity ∈ r of the multilayer structure 10 to a negative value in the frequency band II (approximately 1GHz or less) of the EMC region (noise countermeasure region).
The first structural member 11 forming the laminated structure 10 is made of an electrically conductive material having electron conductivity, which is generally made of metal, for example. However, the first structural member 11 does not necessarily have to be a metal as long as it is an electrically conductive material that is not ion-conductive and hole-conductive but electron-conductive. For example, in addition to metals, carbon, conductive polymers, and the like, or materials in which these are blended with resins, rubbers, elastomers, and the like to impart conductivity, and the like are also available.
The relative dielectric constant ∈ r of the conductive material used for the first structural member 11 is described by a delude model (Drude model) which is a model relating to electron conduction, and as shown in fig. 6, it is positive for frequencies f equal to or higher than the plasma frequency fp (f ≧ fp) and negative for frequencies f lower than the plasma frequency fp (f < fp). In the delude model, the relative dielectric constant ∈ r of a metal is given by the mass of electrons, the charge, and the number of conduction electrons, and the plasma frequency fp is a frequency at which the relative dielectric constant ∈ r becomes 0.
In this case, since the plasma frequency fp is generally in the band of the light region in the metal conductive material used for the first structural member 11, the plasma frequency fp is set in the vicinity of the region of the terahertz wave from the microwave or millimeter wave as shown in fig. 7, and the frequency band I (76.5GHz) of the millimeter wave is slightly lower than the plasma frequency rp and the relative dielectric constant ∈ r has a negative value smaller than 0. In this case, the relative dielectric constant ∈ r has a negative value of-500 or less with respect to the frequency band II (about 1GHz or less) of the EMC region (noise countermeasure region).
When the plasma frequency fp in the frequency band of the light region is set in the vicinity of the frequency band I (76.5GHz) of the millimeter wave region, the number of conductive electrons in the conductive material is limited (reduced), whereby the plasma frequency fp of the conductive material made of a metal can be set in the vicinity of the millimeter wave region from the light region.
In the case of limiting the number of conduction electrons, specifically, if the physical size or area of the conductive material is reduced, the number of conduction electrons of the entire conductive material can be reduced, and therefore, this is possible. Specifically, as shown in fig. 4, the first structural member 11 may be formed in a grid shape, and the conductive material may be geometrically arranged. That is, the area of the first structural member 11 may be reduced to physically limit the number of electrons.
The first structural member 11 is not necessarily a mesh made of metal (hereinafter, this is also referred to as "metal mesh"). For example, the first structural member 11 may be formed in a lattice shape by printing a copper foil pattern on the surface of a polyimide film and etching the copper foil pattern. The material and the manufacturing method of the first structural member 11 may be any material and manufacturing method as long as the desired relative dielectric constant ∈ r can be obtained by limiting the total number of conduction electrons.
Fig. 7 shows the calculation result of the relative dielectric constant ∈ r of the first structural member 11 when the frame forming the grid has a thickness t of 0.2mm, a frame width d of 0.06mm, and an arrangement interval a of 1.2 mm. By making the first structural member 11 in a grid shape and reducing the entire area to limit the number of electrons, as shown in fig. 8, the equivalent relative permittivity ∈ r of the laminated structural body 10 and the equivalent relative permeability μ r become 1, and the plasma frequency fp in the frequency band in the light region can be set in the vicinity of the frequency band I (76.5GHz) in the millimeter wave region. As a result, the relative permittivity ∈ r in the frequency band I (76.5GHz) of the first structural member 11 depends on the permittivity ∈ of the stacked second structural member 12, but the relative permittivity ∈ r is set to be smaller than 0 and larger than-25 as a design value, and preferably to have a negative value of-5 or less, which is on the order of-1 or less and-10 or more. In the frequency band II (about 1GHz or less), the relative dielectric constant ∈ r has a negative value of-500 or less, although it depends on the dielectric constant ∈ of the stacked second structural members 12.
However, the thickness t of the frame, the frame width d, and the arrangement interval a of the grid of the first structural member 11 may be appropriately set in accordance with the desired relative permittivity ∈ r, and any shape such as a circular shape or a triangular shape may be selected. The arrangement pattern of the mesh is not necessarily uniform, and may be set arbitrarily as to the degree of dispersion of the mesh and the like.
The second structural member 12 is a dielectric having a generally positive relative permittivity ∈ r in the millimeter wave frequency band I (76.5 GHz). The second structural member 12 can be applied as long as it has the material strength, workability, and various durability required for a radome, and is preferably low in electrical loss for further improvement of performance. Specifically, the imaginary part ∈ ″ when the complex permittivity represents the permittivity ∈ in the frequency band I (76.5GHz) of the material is preferably small, for example, 0.001 or less, and more preferably 0.005 or less, for the second structural member 12.
In this way, a laminated structure 10 is formed in which at least one layer of the first structural member 11 having a negative relative permittivity ∈ r (-5 or less) in the millimeter wave frequency band I (76.5GHz) and at least one layer of the second structural member 12 having a positive relative permittivity ∈ r in the millimeter wave frequency band I (76.5GHz) are laminated.
As a result, as shown in fig. 8, the equivalent relative permittivity ∈ r of the multilayer structure 10 having the three-layer structure including the two second structures 12 and the one first structure 11 can be matched to 1 in the frequency band I (76.5GHz) of millimeter waves, and the equivalent relative permittivity ∈ r of the multilayer structure 10 can be increased in the negative direction (-500 GHz or less) in the frequency band II (about 1GHz or less) of the EMC region.
Specifically, the equivalent relative permittivity ∈ r in the frequency band I (76.5GHz) of the laminated structure 10 is set to substantially 1, specifically 0.9 to 1.3, and more preferably 1.0, and the equivalent relative permittivity ∈ r in the frequency band II (approximately 1GHz or less) of the laminated structure 10 is set to-370 or less, and preferably-500 or less.
Therefore, the equivalent relative permeability μ r of the laminated structure 10 is the same as the relative permittivity ∈ r, and the wave impedance η 1 of air is the same as the equivalent wave impedance η 2 of the laminated structure 10, and as a result, as shown in fig. 9, the apparent transmittance T of the laminated structure 10 can be realized to be 1 in the frequency band I (76.5 GHz).
Meanwhile, if the ratio of the equivalent relative permeability μ r to the relative permittivity ∈ r of the laminated structure 10 is small, and the relative permittivity ∈ r2 as the denominator is negative and has a large absolute value, the wave impedance η 2 approaches "0", and therefore, the apparent transmittance T in the frequency band II (about 1GHz or less) can be achieved to be 0.
< action and Effect >
In the above configuration, in the millimeter wave radar cover 1, the first structural member 11 having a negative relative permittivity in the millimeter wave frequency band I (76.5GHz) and the second structural member 12 having a positive relative permittivity in the millimeter wave frequency band I (76.5GHz) are laminated by at least one layer to obtain the laminated structural body 10, and the laminated structural body 10 is used as the radome in the first portion a.
The laminated structure 10 protects the internal antenna 30 and the electronic circuit 40 by the second structure 12, and achieves a transmittance T of 1 in the millimeter wave frequency band I (76.5GHz) and a transmittance T of approximately 0 in the EMC frequency band II (approximately 1GHz or less).
Thus, the millimeter wave radar cover 1 can transmit the electromagnetic wave of the millimeter wave from the antenna 30 without the electrical attenuation by the laminated structure 10, and can receive the reflected wave without the electrical attenuation by the laminated structure 10. Meanwhile, the millimeter wave radar cover 1 can suppress the radiation of unnecessary electromagnetic waves in the EMC region via the laminated structure 10, and can prevent the interference and disturbance of electromagnetic waves from other external devices.
< example >
As a specific structure of the laminated structure 10, for example, the first structural member 11 is made of a metal mesh of copper, the second structural member 12 is made of polyimide, both the first structural member 11 and the second structural member 12 have a size of 200 × 200mm, and a three-layer laminated structure is formed in the order of the second structural member 12, the first structural member 11, and the second structural member 12.
The first structural member 11 was fabricated by etching a copper foil having a thickness t of 0.08mm into a grid pattern having a line width d of 0.06mm and a vertical arrangement interval a and a horizontal arrangement interval a of 1.2 mm. The relative dielectric constant ∈ r of the first structural member 11 at this time can be set such that the plasma frequency fp in the frequency band in the light region is set in the vicinity of the frequency band I (76.5GHz) in the millimeter wave region. The second structural member 12 is polyimide having a complex relative dielectric constant of 3.25-j0.001 in the frequency band I (76.5GHz) of millimeter waves, and has a thickness of 0.31 mm.
The laminated structure 10 having a three-layer laminated structure was formed by press molding the second member 12, the first member 11, and the second member 12 in this order under a pressure of 60t using an adhesive. As a result, the thickness of the laminated structure 10 was 0.62 mm. That is, this is a state in which the first structural member 11 is deformed in a state of being sandwiched by the two second structural members 12 and air does not enter between the three layers.
In this case, in the laminated structure 10 having the three-layer laminated structure, the relative permittivity ∈ r, the relative permeability μ r, and the like of the first and second members 11 and 12 are appropriately adjusted so that the transmittance T in the frequency band I (76.5GHz) in which millimeter waves are realized including the adhesive is 1 and the transmittance T in the frequency band II (about 1GHz or less) in the EMC region is approximately equal to 0.
Fig. 8 shows the results of measuring the equivalent relative permittivity ∈ r and relative permeability μ r of the laminated structure 10. As shown in fig. 9, the transmittance T of the laminated structure 10 is 1 in the millimeter wave frequency band I (76.5GHz) and is approximately equal to 0 in the EMC region frequency band II (approximately 1GHz or less).
< Structure of curved laminated Structure >
However, in such a millimeter wave radar cover 1, the millimeter waves are irradiated through the three-layer structure of the laminated structure 10, and the moving speed, distance, size, and the like of the surroundings, particularly the object ahead (for example, an object such as a preceding vehicle or a person), can be detected based on the intensity of the reflected waves, the time difference of the reflected waves, and the like.
In practice, when detecting a forward object (object), scanning is performed while scanning the forward object with an electromagnetic wave of a millimeter wave in a horizontal direction by a physical (mechanical scanning) or electrical (digital beam forming, array antenna, or the like) method. The scanning method is not particularly limited, and the irradiation direction may be changed by physically moving the antenna 30 or by electrically changing the irradiation direction without physically moving the antenna 30.
Thus, the electromagnetic wave of the millimeter wave emitted in the target direction can be reflected by the object in the target direction and then received by the antenna 30, and thus an object (object) existing in a certain range in the horizontal direction in front can be detected.
However, when a reflected wave from an object (object) is received, a millimeter wave from a direction other than the target direction may fly. For example, there is a case where an irradiated wave, a reflected wave, or the like from a so-called multipath (i.e., a propagation path is different depending on the shape of an object (object) and/or a peripheral reflecting object (guardrail, other vehicle, ground surface, or the like)) and/or from a millimeter wave radar other than the vehicle and/or other than the vehicle comes into flight.
In general, in the millimeter wave radar, since the beam width of the antenna 30 is narrowed in order to improve the resolution in the horizontal direction, it is difficult to receive the electromagnetic wave of the millimeter wave from the direction other than the target direction by the antenna 30, but if the electromagnetic wave of the millimeter wave coming in flight intrudes into the millimeter wave radar, the background noise increases, and the detection sensitivity is affected.
Then, as shown in fig. 10, a curved laminated structure 10W is used in the millimeter wave radar, and the curved laminated structure 10W has a structure in which, when an electromagnetic wave of a millimeter wave is irradiated in a target direction at the time of detecting an object (object) in a horizontal direction, an electromagnetic wave of the millimeter wave from a direction other than the target direction is not incident on the millimeter wave radar.
The curved laminated structure 10W has the same basic structure as the above-described laminated structure 10, and is a three-layer structure in which a first structural member 11 and a second structural member 12 sandwiching the first structural member 11 from both the front side (arrow a direction) and the back side (arrow b direction) are laminated. Here, the significant difference between the curved laminated structure 10W and the laminated structure 10 is that: the curved portion is convex as a whole in the outward direction of the front surface side (arrow a direction) away from the antenna 30, which is the emission source of the millimeter wave radar.
The curved laminated structure 10W is characterized in that: has the following oblique incidence transmittance characteristics: when electromagnetic waves of millimeter waves are incident perpendicularly to the laminated structure 10 (hereinafter, this is referred to as "perpendicular incidence"), the transmittance T is high, and when the electromagnetic waves are incident at an angle other than the perpendicular incidence, the transmittance T is low.
Specifically, the curved laminated structure 10W is curved in a convex shape in a direction away from the antenna 30 (outside the radar) so that the electromagnetic wave enters the curved laminated structure 10W perpendicularly to the antenna 30 at any direction of the electromagnetic wave emitting source of the millimeter wave, that is, the antenna 30.
In this case, the curved laminated structure 10W is preferably curved with a semicircular curvature having a radius r0 equal to r1 at any portion around the antenna 30. In the case of such an ideal curved laminated structure 10W, the electromagnetic wave of the millimeter wave radiated from the antenna 30 can be vertically incident on any part of the curved laminated structure 10W, and the electromagnetic wave of the millimeter wave vertically incident on the curved laminated structure 10W from the outside can be received by the antenna 30.
Meanwhile, in the curved laminated structure 10W, reflected waves of millimeter waves from directions other than the vertical incidence direction and/or reflected waves flying through multipath are incident on the curved laminated structure 10W not vertically but in a state of having a certain angle, and therefore, the transmittance T is lowered.
As shown in fig. 11 (a) to (C), when the incident angle of the millimeter wave electromagnetic wave incident on the curved laminated structure 10W is 0 degrees, that is, perpendicular, the transmittance T is 1, and when the incident angle is smaller or larger than 0 degrees, the transmittance T < 1, where the incident angle of 0 degrees means that the millimeter wave electromagnetic wave is incident in a normal state (angle along the normal) in which the millimeter wave electromagnetic wave perpendicularly intersects the tangent to the second structure 12, and when the curved laminated structure 10W is in a semicircular shape having a radius r0 of r1, the millimeter wave electromagnetic wave is perpendicularly incident on the curved laminated structure 10W even when the millimeter wave electromagnetic wave is irradiated from the antenna 30 in a state inclined by α degrees.
However, although the incident angle of 0 degree is a normal line where the electromagnetic waves of the millimeter waves intersect perpendicularly with respect to the tangent of the second structure 12, strictly speaking, even if the incident angle is inclined in the range of ± 2 degrees with respect to the tangent, the incident angle of the electromagnetic waves of the millimeter waves is considered to be perpendicular with respect to the second structure 12.
In this case, the curved laminated structure 10W does not necessarily have to have a semicircular shape with a radius r0 equal to r1, and may have, for example: the overall thickness of the aspherical shape (in this case, the elliptical shape) having the radius r0 < r1 but limited to the degree of inclination in the range of ± 2 degrees with respect to the tangent line is reduced to a small degree of protrusion in a convex shape.
In the curved laminated structure 10W having such a structure, the electromagnetic wave of the millimeter wave radiated from the antenna 30 in the target direction can be transmitted and reach the object. On the other hand, in the curved laminated structure 10W, electromagnetic waves of millimeter waves from directions other than the target direction are not transmitted and do not reach the antenna 30, and therefore, the background noise is not increased, and the detection sensitivity is not affected.
Thus, in the millimeter wave radar, for example, when detecting an object (object) in the horizontal direction while operating the irradiation direction over a wide range of about ± 40 degrees with the antenna 30 as the center, it is possible to prevent the intrusion of the electromagnetic wave of the millimeter wave from the direction in which the object is not present, by the curved laminated structure 10W.
As shown in fig. 11 (a) to (C), when the millimeter-wave electromagnetic wave from the antenna 30 is incident perpendicularly to the second structure 12 of the curved laminated structure 10W, that is, when the millimeter-wave electromagnetic wave is incident perpendicularly to the tangent to the second structure 12, the first structure 11, and the second structure 12, the millimeter-wave electromagnetic wave is transmitted but not transmitted.
Here, "transmission (○)" means that the transmittance T is 0.95 or more, and "non-transmission (×)" means that the transmittance T is less than 0.95, but the present invention is not limited thereto, and the value of the transmittance T may be set arbitrarily in consideration of the application and/or the detection accuracy on the measurement side.
Specifically, as shown in fig. 12, if the incident angle of the millimeter wave electromagnetic wave with respect to the curved laminated structure 10W is 0 degrees, the transmittance T is approximately 1; if the incident angle of the electromagnetic wave of the millimeter wave is shifted by 5 degrees, the transmittance T becomes 0.93, and if shifted by 10 degrees, the transmittance T < 0.8.
The curved laminated structure 10W formed of a three-layer structure having such oblique incidence transmittance characteristics can be realized by appropriately setting the thickness and dielectric constant of the dielectric material in the second structure 12, and the thickness t, line width d, and arrangement interval a in the vertical and horizontal directions of the metal mesh in the first structure 11.
In particular, in order to achieve the desired oblique incidence transmittance characteristics, the thickness t of the metal mesh in the first structural member 11 is important, and is set to 0.5mm to 2.0mm, more preferably 0.8mm to 1.5mm, and other dimensions may be set to desired design values.
As shown in fig. 13, similarly to the curved laminated structure 10W, a dielectric-lens-integrated curved laminated structure 100W having a structure in which, when an electromagnetic wave of a millimeter wave is irradiated in a target direction, the electromagnetic wave of the millimeter wave from a direction other than the target direction is not incident on the millimeter-wave radar (hereinafter, this structure may be referred to as a "dielectric-lens-integrated curved laminated structure") may be used.
In the dielectric-lens-integrated multilayer curved structure 100W, the dielectric lens 20 formed of a convex lens having a predetermined dielectric constant and refracting the electromagnetic wave of the millimeter wave incident from the antenna 30 is disposed between the second structure 12 and the antenna 30 in the multilayer curved structure 10W, and the dielectric-lens-integrated multilayer curved structure 100W is a structure in which the second structure 12 and the dielectric lens 20 are integrated.
The dielectric-lens-integrated multilayer curved structure 100W is integrated with the dielectric lens 20, and refracts millimeter-wave electromagnetic waves inward by the dielectric constant of the dielectric lens 20. Therefore, the dielectric-lens-integrated curved laminated structure 100W can be made vertically incident with the millimeter-wave electromagnetic wave even when the millimeter-wave electromagnetic wave is irradiated from the antenna 30 with a wide angle corresponding to the amount of the millimeter-wave electromagnetic wave, and can be made thin as a whole as in an aspherical shape (in the case of an elliptical shape) having a radius r10 < r 11.
As shown in fig. 14(a) to (C), when the incident angle of the millimeter wave incident on the dielectric lens integrated curved laminated structure 100W is 0 degrees, that is, perpendicular, the transmittance T is 1, and when the incident angle is smaller or larger than 0 degrees, the transmittance T < 1.
Since the dielectric-lens-integrated multilayer curved structure 100W refracts the millimeter-wave electromagnetic wave inward due to the dielectric constant of the dielectric lens 20, the millimeter-wave electromagnetic wave is incident perpendicularly to the dielectric-lens-integrated multilayer curved structure 100W even when the millimeter-wave electromagnetic wave is irradiated from the antenna 30 in a state inclined by α degrees.
In this case, as shown in fig. 15, in the dielectric-lens-integrated multilayer structure 100W, the electromagnetic wave of the millimeter wave incident from the antenna 30 of the internal Rin of the millimeter wave radar cover 1 at the predetermined angle θ 1 with respect to the dielectric lens 20 is slightly refracted inward by the dielectric lens 20 to the angle θ 2, travels inside the dielectric lens 20, and then is irradiated to the outside Rout via the multilayer structure 10W.
Further, by integrally providing the dielectric lens 20 to the dielectric lens integrated curved laminated structure 100W, the degree of protrusion (curvature) in a convex shape can be reduced and the thickness can be further reduced as compared with the case of only the curved laminated structure 10W.
< other embodiments >
Although the preferred embodiments of the present invention have been described above, the present invention is not limited to the millimeter wave radar cover 1 according to the above-described embodiments, and includes all the aspects covered by the concept of the present invention and the claims. Further, at least some of the above problems and effects can be achieved by appropriately and selectively combining the respective configurations. For example, the shape, material, arrangement, size, and the like of each component in the above embodiments may be appropriately changed according to a specific use mode of the present invention.
In the above-described embodiment, the case of using the curved laminated structure 100W integrated with a dielectric lens integrated with the dielectric lens 20 formed of a convex lens has been described, but the present invention is not limited to this, and for example, a curved laminated structure 200W integrated with a dielectric lens 21 formed of a concave lens as shown in fig. 16 (a) and (B) may be used.
Specifically, as shown in fig. 16 (a), the dielectric-lens-integrated multilayer structure 200W is an integrated structure in which a dielectric lens 21 having a predetermined dielectric constant and refracting electromagnetic waves of millimeter waves incident from the antenna 30 through the multilayer structure 10W is laminated on the second structural member 12 on the outer peripheral side of the multilayer structure 10W, and the dielectric lens 21 is a concave lens. The dielectric lens 21 as a concave lens may be curved with the same curvature as the second structural member 12 of the curved laminated structure 10W.
As shown in fig. 16B, in the dielectric-lens-integrated multilayer structure 200W, the electromagnetic wave of the millimeter wave incident perpendicularly (angle θ 1 is 0 degrees) from the tangent line of the antenna 30 to the second structure 12 on the inner peripheral side of the multilayer structure 10W is refracted outward at an angle θ 2(θ 2 > θ 1) when passing through the dielectric lens 21, and is irradiated to the outside Rout. Therefore, the dielectric-lens-integrated multilayer curved structure 200W can emit millimeter-wave electromagnetic waves at a wider angle by integrating the dielectric lens 21 formed by the concave lens, and can be further thinned as a whole.
Industrial applicability of the invention
The cover for millimeter wave radars according to the present invention is used not only for vehicles such as automobiles but also for mobile devices such as railways, aircrafts, and ships and is also applicable to fields such as electric and electronic devices and other industrial machines.
Description of the reference numerals
1 … millimeter wave radar cover, 10 … laminated structure, 10a … surface, 10B … inner surface, 11 … first structure, 12 … second structure, 20, 21 … dielectric lens, 30 … antenna, 40 … electronic circuit, a … first portion, B … second portion, 10W … curved laminated structure, 100W, 200W … dielectric lens integrated curved laminated structure.

Claims (5)

1. A cover for a millimeter wave radar that accommodates a millimeter wave radar including an antenna and an electronic circuit that drives the antenna, characterized by comprising:
a first portion that protects the millimeter wave radar and is provided on a front surface of the millimeter wave radar so as to transmit an electromagnetic wave of a millimeter wave emitted from the antenna; and
a second portion having a housing space for housing the antenna and the electronic circuit except for the first portion,
the first portion includes a laminated structure in which at least one layer of a first structural member having a negative dielectric constant in the millimeter wave band and at least one layer of a second structural member having a positive dielectric constant in the millimeter wave band are laminated,
the laminated structure is curved in a convex shape in a direction away from the emission source of the millimeter wave electromagnetic wave.
2. The millimeter-wave radome of claim 1, wherein the reflector is a reflector for reflecting the millimeter-wave radiation,
the multilayer structure has an apparent transmittance of about 1 only when the millimeter-wave electromagnetic wave is incident perpendicularly.
3. The millimeter wave radome of claim 1 or 2, wherein the millimeter wave radar cover is a millimeter wave radar cover,
the laminated structure is integrated with a dielectric lens having a predetermined dielectric constant and refracting the electromagnetic wave of the millimeter wave incident from the emission source.
4. The millimeter-wave radome of claim 1, wherein the reflector is a reflector for reflecting the millimeter-wave radiation,
the first structural member is formed by geometrically arranging a conductive material, and when the first structural member and the second structural member are laminated, the apparent transmittance of the laminated structure is a value near 1 with respect to the millimeter wave band.
5. The millimeter wave radome of claim 1 or 4, wherein the reflector is a reflector for reflecting the millimeter wave radiation,
the multilayer structure has an apparent transmittance of a value in the vicinity of 0 for a frequency band of the electromagnetic compatibility region lower than the frequency band of the millimeter wave.
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Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102019204700A1 (en) * 2019-04-02 2020-10-08 Brose Fahrzeugteile Se & Co. Kommanditgesellschaft, Bamberg Radar device, method for manufacturing a radar device and motor vehicle
CN112701480B (en) * 2019-10-22 2023-05-05 Oppo广东移动通信有限公司 Antenna device and electronic equipment
KR20210077033A (en) * 2019-12-16 2021-06-25 현대자동차주식회사 Transmission moudle of electromagnetic wave of radar for vehicle
FR3111711A1 (en) * 2020-06-19 2021-12-24 Valeo Vision Vehicle assembly including radar sensor
CN112332090B (en) * 2020-10-23 2022-01-04 捷开通讯(深圳)有限公司 Antenna structure and mobile terminal
CN113267748A (en) * 2021-04-09 2021-08-17 陈昱 PC/PBT wave-transparent plate based on esterification technology

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56137703A (en) * 1980-03-28 1981-10-27 Nec Corp Branching and filtering method for electromagnetic wave
JP2516293Y2 (en) * 1991-04-24 1996-11-06 三菱電機株式会社 Array antenna device
JPH11248835A (en) * 1998-02-27 1999-09-17 Mitsubishi Electric Corp Radio-wave radar apparatus
WO2009107684A1 (en) * 2008-02-26 2009-09-03 旭硝子株式会社 Artificial medium
JP2015053661A (en) * 2013-09-09 2015-03-19 日本電信電話株式会社 Antenna device and reflector arrangement method
JP2016145777A (en) * 2015-02-09 2016-08-12 株式会社デンソー Radar device loading structure
JP2017015474A (en) * 2015-06-30 2017-01-19 株式会社日立製作所 Railway vehicle control system

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004077399A (en) * 2002-08-22 2004-03-11 Hitachi Ltd Milliwave radar
US8350777B2 (en) * 2010-02-18 2013-01-08 Raytheon Company Metamaterial radome/isolator
JP5582201B2 (en) 2013-01-21 2014-09-03 三菱エンジニアリングプラスチックス株式会社 Millimeter wave radar cover and millimeter wave radar
CN106935970B (en) * 2015-12-31 2021-09-03 深圳光启高等理工研究院 Metamaterial structure, radome, antenna system and method for forming sandwich structure
JP7159049B2 (en) 2016-09-08 2022-10-24 Nok株式会社 Cover for millimeter wave radar

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56137703A (en) * 1980-03-28 1981-10-27 Nec Corp Branching and filtering method for electromagnetic wave
JP2516293Y2 (en) * 1991-04-24 1996-11-06 三菱電機株式会社 Array antenna device
JPH11248835A (en) * 1998-02-27 1999-09-17 Mitsubishi Electric Corp Radio-wave radar apparatus
WO2009107684A1 (en) * 2008-02-26 2009-09-03 旭硝子株式会社 Artificial medium
JP2015053661A (en) * 2013-09-09 2015-03-19 日本電信電話株式会社 Antenna device and reflector arrangement method
JP2016145777A (en) * 2015-02-09 2016-08-12 株式会社デンソー Radar device loading structure
JP2017015474A (en) * 2015-06-30 2017-01-19 株式会社日立製作所 Railway vehicle control system

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